Commonwealth legislation

AD/BAe 146/36 Amdt 1 - Wing to Fuselage Fairings

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legislative instrument

Plain English Summary

5/10 complexity

Mandates specific inspections of wing-to-fuselage fairings on BAe 146 aircraft that have modification HCM00301A or B but do not have HCM01698A, requiring work in accordance with BAE Systems Service Bulletins ISB 53-005 Revision 2 and ISB 53-067 Revision 3 (or later EASA‑approved revisions). Inspections must be done before 1,000 landings since new (or 500 landings after 29 Sep 2005), and before every 4,000 landings since the last inspection, with repeat intervals set by the service bulletins. The change responds to reported fuselage skin chafing and updates prior directives to maintain structural integrity.

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Direct links to the current provisions in AD/BAe 146/36 Amdt 1 - Wing to Fuselage Fairings.

British Aerospace BAe 146 Series Aeropla

British Aerospace BAe 146 Series Aeroplanes

AD/BAe 146/36 Amdt 1	Wing to Fuselage Fairings	10/2005

Applicability:	All Model BAe 146 series aircraft with modification HCM00301A or B incorporated and without modification HCM01698A (SB 53-162-01698A Protective Tape and Sealant) incorporated.
Requirement:	1. For aircraft not previously inspected in accordance with BAE Systems Operations Ltd Service Bulletin (SB) ISB 53-005 and/or ISB 53-067: Perform the inspection detailed in SB ISB 53-005 Revision 2 and ISB 53-067 Revision 3, or later EASA approved revisions.2. For aircraft previously inspected in accordance with SB ISB 53-005 and ISB53-067: Perform the inspections detailed in SB ISB 53-005 Revision 2 and ISB 53-067 Revision 3, or later EASA approved revisions.Note: UK CAA AD G-2005-0020 refers.
Compliance:	1. Before the accumulation of 1,000 landings since new, or 500 landings after 29 September 2005, whichever occurs later. Thereafter, repeat the inspections at the intervals specified in the requirement document.2. Before the accumulation of 4,000 landings since the last inspection. Thereafter, repeat the inspections at the intervals specified in the requirement document.
	This Amendment becomes effective on 29 September 2005.
Background:	Chafing of the fuselage skin has been reported.

Amendment 1 is issued in response to a new CAA AD, which introduces the latest revisions of SB ISB 53-005 and ISB 53-067. Inspection of the affected chafing areas was originally mandated by CAA ADs 002-09-84 (AD/BAe 146/1) and 009-12-87 (this Directive). In order to ensure the continued airworthiness for life extension it was necessary to review the corrective actions required by the above CAA ADs. As a result of this review it has been determined that the related service bulletins needed to be revised to assure the continued structural integrity of the fuselage.

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David Villiers
Delegate of the Civil Aviation Safety Authority

8 August 2005

AD/BAe 146/36 Amdt 1

Wing to Fuselage Fairings

10/2005

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

British Aerospace BAe 146 Series Aeropla British Aerospace BAe 146 Series Aeroplanes

British Aerospace BAe 146 Series Aeroplanes

AD/BAe 146/36 Amdt 1	Wing to Fuselage Fairings	10/2005

Applicability:	All Model BAe 146 series aircraft with modification HCM00301A or B incorporated and without modification HCM01698A (SB 53-162-01698A Protective Tape and Sealant) incorporated.
Requirement:	1. For aircraft not previously inspected in accordance with BAE Systems Operations Ltd Service Bulletin (SB) ISB 53-005 and/or ISB 53-067: Perform the inspection detailed in SB ISB 53-005 Revision 2 and ISB 53-067 Revision 3, or later EASA approved revisions.2. For aircraft previously inspected in accordance with SB ISB 53-005 and ISB53-067: Perform the inspections detailed in SB ISB 53-005 Revision 2 and ISB 53-067 Revision 3, or later EASA approved revisions.Note: UK CAA AD G-2005-0020 refers.
Compliance:	1. Before the accumulation of 1,000 landings since new, or 500 landings after 29 September 2005, whichever occurs later. Thereafter, repeat the inspections at the intervals specified in the requirement document.2. Before the accumulation of 4,000 landings since the last inspection. Thereafter, repeat the inspections at the intervals specified in the requirement document.
	This Amendment becomes effective on 29 September 2005.
Background:	Chafing of the fuselage skin has been reported.

David Villiers
Delegate of the Civil Aviation Safety Authority

8 August 2005

AD/BAe 146/36 Amdt 1 - Wing to Fuselage Fairings

Plain English Summary

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Current sections

British Aerospace BAe 146 Series Aeroplanes

British Aerospace BAe 146 Series Aeroplanes